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Liquid propellant rocket combustion instability
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Author and Affiliation:
Harrje, D. T.(NASA, Washington, DC, United States)
Abstract: The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
Publication Date: Jan 01, 1972
Document ID:
19720026079
(Acquired Nov 22, 1995)
Accession Number: 72N33729
Subject Category: PROPELLANTS
Report/Patent Number: NASA-SP-194
Document Type: Technical Report
Publisher Information: United States
Financial Sponsor: NASA; United States
Organization Source: NASA; Washington, DC, United States
Description: 657p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: COMBUSTION STABILITY; LIQUID PROPELLANT ROCKET ENGINES; PROBLEM SOLVING
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